APOLLO Cryogenic Integrated Systems Program Programmers Guide
In-Space Propellant Systems Safety. Volume 1 Executive Summary
Numerical Simulation of the Thermal Effect in the Cavitating Venturi Flow
Reusable Subsystems Design/Analysis Study. Volume 2. Part A. Technical Study Report
Role of Ignition Delay in Rotating Detonation Engine Performance and Operability
Multidisciplinary Design and Architecture Optimization of a Reusable Lunar Lander
Timescale-Based Frozen Nonadiabatic Flamelet Combustion Modeling for Rocket Engine Thrust Chambers
In-Space Propellant Logistics. Volume 4 Project Planning Data
Preliminary Assessment of Using Gelled and Hybrid Propellant Propulsion for VTOL/SSTO Launch Systems
Cryogenic Propellant Production Depot for Low Earth Orbit
Characteristics of Thermal Cavitation on a Two-Dimensional Hydrofoil